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SBIR/STTR

Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems, Phase II

Completed Technology Project

Project Introduction

Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems, Phase II
The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a proven existing solver called Loci-STREAM which has been developed by the proposing personnel under fu More »

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